Study of Stability of Rotational Motion of Spacecraft with Canonical Variables

Table 5

Analysis of possible singularities of the Anloyer variables for satellites MP, PP1 of and PP2.

Lyapunov stable equilibrium point of Table 2, 3 and 4, respectively.
Satellite	𝐼2(rad)	𝐽2(rad)	𝜔(rad/s)	𝑇(s)	Situation
MP	2,20566	0,862451	0,00373909	1680,4	Accepted
PP-1	1,03788	1,55784	1,59939	3,92848	Accepted
PP-2	1,26592	1,48439	0,196422	31,9882	Accepted